An aircraft is flying along a straight horizontal path at 200 m s'. The pilot tilts the wings through an angle of 10'. What is the radius of circular path, which the plane will follow?

The ratio of lift to drag l/d for a wing or airfoil is an important aerodynamic parameter, indeed, it is a direct measure of the aerodynamic efficiency of the wing. if a wing is pitched through a range of angle of attack, l/d first increases, then goes through a maximum, and then decreases. consider an infinite wing with an naca 2412 airfoil. estimate the maximum value of l/d. assume that the reynolds number is 9x10^6.

What’s #16 asking me and how do i solve it?

Complete the sentence to describe the law of conservation of energy. the law of conservation of energy states that energy cannot be created